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Composite Materials Research Progress

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244<br />

Maria Pia Cavatorta and Davide Salvatore Paolino<br />

events [40]. Strictly speaking, the DD is not a damage variable but rather a point by point<br />

measurement of the laminate efficiency of energy absorption, whereas the coefficient η<br />

proposed by Liu averages the efficiency of energy absorption over a wide range of impact<br />

energies (from very low energies to Pn).<br />

E a/P n<br />

1<br />

0.9<br />

0.8<br />

0.7<br />

0.6<br />

0.5<br />

0.4<br />

0.3<br />

0.2<br />

0.1<br />

0<br />

GVP90_12.31<br />

GE90s_8.00<br />

GE90m_8.00<br />

GE45_4.50<br />

GE90s_4.00<br />

GE90m_4.00<br />

CE60_1.75<br />

CE90_1.55<br />

CE60_0.85<br />

CE90_0.75<br />

CE60_0.40<br />

CE90_0.35<br />

0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0<br />

E i/P n<br />

Figure 3. Energy absorption Master Curve.<br />

Figure 3 plots the Master Curve proposed in [19]. Data for the three thicker laminates are<br />

again superimposed and very close to the bisector, meaning that the absorbed energy is about<br />

equal the impact energy (DD almost one). For thin laminates, the difference is more enhanced<br />

pointing out a lower efficiency of energy absorption [3].<br />

As said, no indications can be evinced from Figures 2 and 3 in terms of laminate damage<br />

tolerance. In this respect, definition of the DuI, which differentiates between the nature of<br />

energy absorption mechanisms, appears rather appealing. In its original definition, the DuI is<br />

meant to rank different laminates tested under similar impact conditions, on the basis of a<br />

more fragile or more ductile behavior under impact loading. It is worthwhile noticing that in<br />

the literature the DuI is basically used to rank different laminates at perforation or fracture<br />

(Charpy tests), for which determination of Einitiation and Epropagation poses no trouble. The forcedisplacement<br />

curves are open curves and Einitiation is calculated without ambiguity as the area<br />

bounded by the force-displacement curve up to Fpeak and the horizontal axis, while Epropagation<br />

is calculated as the area bounded by the force-displacement curve from Fpeak to a constant<br />

level of force and the horizontal axis (Figure 4a). In the attempt of proving the DuI against<br />

other damage variables, computation of the DuI was also applied to impact tests with<br />

rebound. When the dart rebounds, the force-displacement curves are closed curves and<br />

computation of Einitiation and Epropagation becomes troublesome as different areas could be<br />

considered. No references of DuI computation in impact tests with rebound were found in the<br />

literature. Considering that in impact events with rebound the energy absorbed by the<br />

laminate is equal to the area bounded by the force-displacement curve, in computing the DuI

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